huangyhg

aircraft loads
hi :
i am trying to check the strength of fail safe chord of a aircraft frame. i know the axial load on the skin creates moment on the frame. but i want to know what are the loads and moment acting on the inner and failsafe chord.
thanks
eng-tips forums is member supported.
see your fem results ...
not a helpfull answer, i know, but geez no-one can answer the question sensibly.
sensibly the fail-safe chord is designed by limit loads for the failed structure cases, but somehow i don't think that'll help you either.
good luck

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